Lab Description

Gallery of Research

  • Harper Memorial Wind Tunnel
  • Machine Learning Blade Vortex Map
    Rotor Blade Wake from Machine Learning Based Model
  • Ducted Fan Flow Dynamics
    Ducted Fan PIV Flow Field
  • PIV of Ducted Fan
    Ducted Fan PIV
  • Ducted Fan Research Setup
    Ducted Fan Experimental Setup
  • CFD of Circuit Breaker Fluid Dynamics
    Fluid Dynamics within High Voltage Circuit Breaker
  • CFD of Quadrotor
    LBM-generated UAV Flow Dynamics
  • Real-Time LBM-generated Ship-Deck Landing Flow Dynamics
  • PIV Setup over Ship in Wind Tunnel
    Ship Airwake and Rotor Interaction Experimental Setup
  • PIV Flow Field over Ship
    Experimental Ship Airwake PIV
  • PIV Laser over Ship
    Ship Airwake and Rotor Interaction PIV Setup
  • Rotor-Wing Interaction Experimental Setup
  • Rotor-Rotor Interaction Experimental Setup
  • Ground Effect Research Setuo
    Rotor-Boundary Interaction Experimental Setup
  • Adaptive Flutter Supression Experimental Setup
  • Proprotor-Wing Aerodynamic Interactions Experimental Setup
  • Proprotor-Wing Aerodynamic Interactions Experimental PIV
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About

Directed by Prof. Juergen Rauleder, this lab focuses on both the computational and experimental sides of aerodynamics and fluid mechanics. The focus is on highly-efficient (up to real-time) flow field computations and unsteady, time-resolved, high-speed measurements of velocity fields, forces, and pressures. Of current interest are interactional and configuration aerodynamics, aero-propulsive interactions, coupled aerodynamics with flight dynamics, new (distributed) propulsion concepts, as well as fluid-structure interactions as applied to all aspects of active and passive rotating and fixed-wing systems. The lab’s basic research is applied to the aerodynamic design, optimization, and understanding of current and future fixed-wing aircraft and vertical lift configurations, including advanced and urban aerial mobility and UAS, as well as pilot training and simulators. The research is sponsored by the U.S. Army, Navy, NASA, ONR, NATO, the EU, and by industry. 

State-of-the-art computational and experimental infrastructure includes several GPU computing clusters, high-speed Particle Image Velocimetry (PIV) systems for optical flow field measurements, concurrent structural deformation measurement using Digital Image Correlation (DIC), 6-DOF force/torque sensors and unsteady pressure sensors. Most of the experiments are done in Georgia Tech’s John J. Harper Wind Tunnel (with a 7×9 foot test section) and the two-story high Hover Chamber in the Indoor Flight Lab (IFL).